# SDR YENA2026070900555

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 5, 2026
- Submitted: July 10, 2026
- Operation: Air carrier
- Aircraft: [N568JB](https://openairdocs.org/aircraft/N568JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02063
- Aircraft time: 84,031 hours, 30,499 cycles
- System (JASC): [5315 · Fuselage Main, Floor Beam](https://openairdocs.org/jasc/5315)
- Part: Floorbeam
- Condition: Cracked
- Location: Zone 200
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/YENA2026070900555

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOOR BEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 2 ZONE 2 CRACK LENGTH IS 0 .650 INCH APPROX, IN FWD CARGO COMPARTMENT (1 EA);  REF AEROMAN NR 2026-299175 WO 2026 196/1 ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT
 LEVEL FR36 (Y765) (RADIUS ON ZONE 2) I.A.W. AEROMAN EA 57-0036-26, REV 0 (COVER PLUS PART 1 AND  PART 2), AIRBUS RDAF 81801723/003/2026, ISSUE A, EC NO. A26-513-01. MEASURE OF CRACK LENGTH IS  0.650 INCH. PERFORMED HFEC AND ROTOTEST ON AFFECTS AREAS AS PER NTM 51-10-08 AND NTM 51-10-01 NO  CRACK INDICATION FOUND,

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